Bending mode acceleration influence on pilot control of flexible booster dynamics.

Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S.

Bibliographic Details
Main Author: Kilpatrick, Philip Stark
Other Authors: Laurence R. Young.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2014
Subjects:
Online Access:http://hdl.handle.net/1721.1/83674
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author Kilpatrick, Philip Stark
author2 Laurence R. Young.
author_facet Laurence R. Young.
Kilpatrick, Philip Stark
author_sort Kilpatrick, Philip Stark
collection MIT
description Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S.
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institution Massachusetts Institute of Technology
language eng
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spelling mit-1721.1/836742019-04-10T23:48:19Z Bending mode acceleration influence on pilot control of flexible booster dynamics. Kilpatrick, Philip Stark Laurence R. Young. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics Aeronautics and Astronautics Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1966. M.S. Lacking p.35 and p.36. Bibliography: p. 45. M.S. 2014-01-09T19:43:43Z 2014-01-09T19:43:43Z 1966 Thesis http://hdl.handle.net/1721.1/83674 26019426 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 x, 94 p. application/pdf Massachusetts Institute of Technology
spellingShingle Aeronautics and Astronautics
Kilpatrick, Philip Stark
Bending mode acceleration influence on pilot control of flexible booster dynamics.
title Bending mode acceleration influence on pilot control of flexible booster dynamics.
title_full Bending mode acceleration influence on pilot control of flexible booster dynamics.
title_fullStr Bending mode acceleration influence on pilot control of flexible booster dynamics.
title_full_unstemmed Bending mode acceleration influence on pilot control of flexible booster dynamics.
title_short Bending mode acceleration influence on pilot control of flexible booster dynamics.
title_sort bending mode acceleration influence on pilot control of flexible booster dynamics
topic Aeronautics and Astronautics
url http://hdl.handle.net/1721.1/83674
work_keys_str_mv AT kilpatrickphilipstark bendingmodeaccelerationinfluenceonpilotcontrolofflexibleboosterdynamics